JASC 5300
Service difficulty reports · 8,206
Reports filed under 5300 · Fuselage Structure (General), newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5300' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5300' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR GAIA01255STSkin · corrodedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BULGING SKIN, POPPED FASTENER HEADS, CORROSION ALONG STRINGER 24L, BS 294-310. ACCOMPLISHED FUSELAGE SKIN LAP REPAIR AT BS 294-310, STRINGER 24L IAW B727 SRM 53-30-3 FIG 5. (M)SDR GAIA01253STWeb · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 178 BULKHEAD CRACKED AT RBL 2, WL 198, ALSO STIFFENERS (HORIZONTAL) ABOVE WL 200 AND BELOW WL 196 ARE CRACKED AT RBL 5. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR AND STIFFENERS REPLACEMENT WL 196-200, SDR GAIA01251STFrame · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED C-3 CARGO DOOR CUT OUT FORWARD OUTBOARD CHORD IS CRACKED 1.5 INCH BS 1090, STRINGER 24R. ACCOMPLISHED BS 1090 FRAME REPAIR AT STRINGER 24R IAW B727 SRM 53-10-2 FIG 5 AND SRM 51-40-3 FIG 1. (M)SDR GAIA01250STWeb · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 178 BULKHEAD WEB IS CRACKED AT APPROXIMATELY WL 218, LBL 12 (POSITION 1L PER W/C 2210). ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR AT LBL 12, WL 218 (POSITION 1L) PER KHA W/C 2210. (M)SDR GAIA01249STAngle · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED C-2 DOOR CUT OUT FORWARD FRAME LOWER STANCHION ADAPTER ATTACH ANGLE BROKEN AT BS 950E, STRINGER 26R. ACCOMPLISHED STANCHION ADAPTER ATTACH ANGLE REPLACEMENT BS 950E, STRINGER 26R IAW B727 SRM 53-10-2 FISDR GAIA01246STSeat TrackDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED SEAT TRACK AT BS 520-540, LBL 45.5 HAS ELONGATED HOLES. ACCOMPLISHED SEAT TRACK REPLACEMENT AT BS 480-550, LBL 45.5 IAW B727 SRM 53-10-5 FIG 1. (M)SDR GAIA01237STWeb · corrodedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED WEB AT BS 328 LBL 45 CORRODED, FLIGHTSTAR AIRCRAFT SERVICES, INC. ACCOMPLISHED FLOORWEB REPLACEMENT BS 295-351, LBL 15-45 IAW B727 SRM 51-40-2 AND SRM 53-10-2 FIG 2. (M)SDR GAIA01236STWeb · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 620 FRAME FORWARD WEB CRACKED THROUGH SEAL RETAINER FASTENER HOLES ABOVE STRINGER 25 RT. ACCOMPLISHED BS 620 FRAME WEB REPAIR AT STRINGER 2R IAW B727 SRM 51-40-2 FIG 1 AND SRM 53-10-2 FIG 3. (M)SDR GAIA01235STAngle · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN THE AFT AIRSTAIR, THE LOWER TORQUE BOX TO BS 1342 LOWER SPANWISE CHORD STIFFENER ATTACH ANGLE IS CRACKED AT BS 1338, RBL 20, WL 200. ACCOMPLISHED STIFFENER ATTACH ANGLE REPLACEMENT BS 1338, RBL 20, WSDR GAIA01234STStringer · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15L CRACKED AT FORWARD END OF LEFT WING SCANNING LIGHT BS 720B PLUS 5. ACCOMPLISHED STRINGER 15L REPAIR AT BS 720B PLUS 5 IAW B727 SRM 53-10-3 FIG 5. (M)SDR GAIA01233STStringer · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15L CRAKED AT AFT END OF LEFT WING SCANNING LIGHT BS 720B PLUS 15. ACCOMPLISHED STRINGER 15L REPAIR AT BS 720B PLUS 15 IAW B727 SRM 53-10-3 FIG 5. (M)SDR GAIA01232STFrame · dentedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 720 FRAME DENTED IN RADIUS BETWEEN STRINER 16-17 LEFT. ACCOMPLISHED BS 720 FRAME REPAIR AT STRINER 16-17L IAW B727 SRM 53-10-2 FIG 3 AND SRM 51-40-3 FIG 1. (M)SDR GAIA01231STStringer · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15R CRACKED AT FORWARD END OF WING SCANNING LIGHT CUT OUT BS 720B PLUS 5. ACCOMPLISHED STRINGER 15R REPAIR AT BS 720B PLUS 5 IAW B727 SRM 53-10-2 FIG 5. (M)SDR GAIA01230STFrame · dentedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN AFT CARGO FRAME BS 1110 HAS A DENT AT STRINGER 26L. ACCOMPLISHED BS 1110 FRAME REPAIR AT STRINGER 26L IAW B727 SRM 51-40-3 FIG 1 AND SRM 53-40-2 FIG 5. (M)SDR GAIA01229STFrame · dentedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN FORWARD CARGO FRAME BS 720 HAD A DENT BELOW STRINGER 25R. ACCOMPLISHED BS 720 FRAME REPAIR AT STRINGER 25R IAW B27 SRM 51-40-3 FIG 1 AND SRM 53-10-2 FIG 3. (M)SDR GAIA01228STFrame · dentedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN FORWARD CARGO FRAME BS 720 HAS 2 DENTS AT STRINGER 25L. ACCOMPLISHED BS 720 FRAME REPAIR AT STRINGER 25L IAW B727 SRM 51-40-3 FIG 1 AND SRM 53-10-2 FIG 3. (M)SDR AALA20011412StringerTUL - FOUND RIVETS HEADS POPPED AND SKIN BULGED AT STRINGER 21R JUST AFT OF STRINGER 440. REMOVED CORRODED SECTION OF STRINGER 21R AND INSTALLED STRINGER SPLICE PER SRM 53-10-3. (M)SDR AALA20011404Stringer · corrodedTUL - FOUND CORROSION IN BOTTOM OF STRINGER 26R. REPAIRED STRINGER PER SRM SB 53-10-3 AND BOTTOM WITH BOLTS, NUTS AND WASHERS THRU STRINGER CLIP AND STRINGER SIDES. (M)SDR USAA010773SkinCLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY INSTALLED DOUBLER 8.5 INCHES BY 11.5 INCHES, BS 1620, BETWEEN S17L AND S19L. DOUBLER INSTALLED PER EA 66107-A, SRM 53-60-01 FIG 101 AND 53-00-01 FIG 204. (M)SDR USAA010772SkinCLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY INSTALLED DOUBLER 2.5 INCHES BY 3 INCHES, BS 423, BETWEEN S16L AND S17L. DOUBLER INSTALLED PER SRM 53-00-01, FIG 206. (M)SDR USAA010771Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED IN TWO PLACES .5 INCH EACH, BS 1620, S18R. REMOVED AND REPLACED TIE CLIP PER SRM 51-40-00. (M)SDR USAA010769SkinCLT - FOUND SKIN PREVIOUSLY INSTALLED DOUBLER, BS 902, S3R. DOUBLER INSTALLED PER SRM 53-00-01, FIG 203. (M)SDR USAA010768Frame · dentedCLT - FOUND FRAME DENTED .5 INCH DIAMETER, BS 1540, OUTBOARD OF S26L. DAMAGE REMOVED, FABRICATED AND INSTALLED DOUBLER AND STRINGER TIE CLIPS PER TR 53-60-01, AND EA 69860. (M)SDR AALA20011406Skin · crackedTUL - FOUND FUSELAGE SKIN CRACKED AT STATION 235 STRINGER 22L. REPAIRED CRACK PER SRM 53-30-3 FIG 3 SHEET 4, CLOSE TO EXISTING REPAIR DOUBLER. INCORPORATED ONE LARGE DOUBLER 16 INCHES BY 8 INCHES TO COVER BOTH AREAS. (M)SDR USAA010800Skin · crackedPIT - FOUND SKIN CRACKED .5 INCH, STATION 1437 L3L. CUT OUT DAMAGE, INSTALLED DOUBLER AND FILLERS PER SRM 53-04 FIG 27. (M)SDR AALA20011408Stringer · corrodedTUL - FOUND CORROSION ON STRINGER 23R STATION 720E. REPLACED STRINGER SECTION 720D PLUS 10 TO 720E PLUS 10 SPLICED EPR SRM 53-10-3 FIG 1. (M)SDR DHL2001803544FittingMAIN CARGO JOINT FITTING WITH INTERCOSTAL L-22.RH SHOWS 5 IN BREAK AT STA FS 834.000.REMOVED BROKEN FITTING PER SRM 51-1-20D.PG 21.CLEANED TREATED AND PRIMED PER SRM 51-18B.INSTALLED NEW FITTING PER SRM51-1-20D PG 9SDR AALA20011353Web · crackedTUL - FOUND CRACKS IN STATION 870 WEB EXTENDING FROM FASTENER BELOW LOAD CONTROL VALVE ON BULKHEAD. INSTALLED REPAIR DOUBLER PER SRM 53-10-02. (M)SDR USAA010779Web · crackedCLT - FOUND WEB CRACKED .5 INCH, BS 178 WL 207 AT RIGHT SIDE CHORD. DAMAGE REMOVED, INSTALLED DOUBLER PER EO 5300V157. (M)SDR USAA010802SkinPIT - FOUND SKIN WITH HEAT DAMAGE 8 INCH BY 12 INCH AREA, STATION 27026-27526 STRINGER 46-50. REMOVED HEAT DAMAGE, INSTALLED REPLACEMENT SKIN/DOUBLER PER EA 54649 AND TYP REPAIR 53-40-01. (M)SDR GAIA01254STWeb · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WS DISCOVERED VERTICAL CRACK NOSE WHEEL WELL LEFT WEB BS 260, WL 160. ACCOMPLISHED WEB REPAIR BS 260, WL 160 IN LEFT NWW IAW B727 SRM 51-40-2 FIG 1 AND SRM 53-10-2 FIG 2. (M)SDR AWXA0001913Skin · puncturedD: 1.5" x 1.5" hole in fuselage below & fwd of L-4 door below STR 21LC: repaired per E.R. 19-5331-01171-DL3SDR USAA010849Angle · crackedPIT - FOUND ANGLE CRACKED 3 INCHES, STATION 294.5 RIGHT WL 208.1 CREASE BEAM TO FLOOR STRUCTURE. REPLACED ANGLE PER T/R. (M)SDR AALA20011366Skin · crackedTUL - FOUND FUSELAGE SKIN CRACKED, EXTENDING FROM WIRE BUNDLE ACCESS HOLE DOWN THROUGH AFT LOWER BOLT HOLE. STOP DRILLED CRACK, NDT CHECKED, AND INSTALLED A TITANIUM DOUBLER PER SRM 53-30-3. (M)SDR USAA010854Angle · corrodedPIT - FOUND ANGLE CORRODED 1 INCH BY 18 INCH AREA, FORWARD SIDE FLOORBEAM STATION 270, WL 207.5 COCKPIT ENTRANCE. CORROSION LEVEL 1, TASK NR C53-107-01. REMOVED CORRODED HORIZONTAL FLANGE FROM Z-CHORD, REPLACED WITH REPAIR ANGLE PER EA 71097. (M)SDR USAA010763Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCH, BS 727D, STRINGER 23R. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-60-03. (M)SDR AALA20011380Seat Track · corrodedTUL - FOUND CORROSION ON NR 3 SEAT TRACK STATION 1194 AROUND SCREW HOLE SEAT TRACK FLANGE. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP PER 53-20-00-13 SRM. (M)SDR AALA20011378Beam · corrodedTUL - FOUND CORROSION ALONG LONGERON 28 LOWER DOOR CUTOUT BEAM AFT CARGO. INSTALLED REPAIR DOUBLER PER SRM 53-10-00-3 FIG 2. (M)SDR RRXA11323Frame · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FRAME AT STA.55 AND L24R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-11, 53-SDR AALA20011393Web · corrodedTUL - FOUND CORROSION STATION 218 RBL 12. INSTALLED DOUBLER PER AARD 53-00-00-02. (M)SDR AALA20011357Frame · crackedTUL - FOUND FRAME 1485 IS CRACKED ON RIGHT SIDE OF STAIRS CUTOUT AT STAIR ACT CASTING. CUT OUT DAMAGED SECTION OF FRAME. INSTALLED REPAIR AS PER AARD 53-10-00-33. (M)SDR AALA20011359Skin · dentedTUL - FOUND DENT ON LEFT SIDE OF AIRCRAFT BELOW FIRST PLUGGED WINDOW, APPROX 3 FEET BELOW RED STRIPE. CUT OUT ONE INCH HOLE TO REMOVE DAMAGE AND INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)SDR UIEA01070Frame · crackedDURING INSPECTION, FOUND FRAME WEB AND DOUBLER STATION 440 CRACKED AT STRINGER 13R, CRACK ENDS IN EXISTING FASTENER LOCATION. PERFORMED OPEN HOLE HFEC INSPECTION TO ENSURE CRACK CONTAINMENT. FABRICATED DOUBLERS AND FILLERS. INSTALLED PER STANDARD PRACTICES SDR UIEA01069Frame · crackedDURING INSPECTION, FOUND FRAME WEB STATION 220 CRACKED AT STRINGER 14R, 1.2 INCH COMMON TO THE TRIANGULAR CUTOUT. STOP DRILLED CRACK. PERFORMED OPEN HOLE HFEC INSPECTION TO ENSURE CRACK CONTAINMENT IN STOP HOLE. FABRICATED DOUBLER AND INSTALLED PER STANDARDSDR UIEA01065Doubler · crackedDURING INSPECTION, FOUND FRAME STATION 420 CRACKED AT STRINGER 14 (E)L AND STRINGER 15L AT THE SHEAR DOUBLER COMMON TO THE STRINGER CUTOUT. TRIMMED AWAY TWO FASTENER ROWS OF THE OUTBOARD REINFORCING ANGLE. STOP DRILLED CRACKS. FABRICATED FILLER, DOUBLERS ANSDR UIEA01064Frame · crackedDURING HFEC INSPECTION, FOUND FRAME STATION 800 CRACKED AT STRINGER 17R COMMON TO THE AFT INNER CHORD AT A FASTENER HOLE. TRIMMED OUT CRACK. FABRICATED FILLER AND REPAIR STRAPS AND INSTALLED PER STANDARD PRACTICES IAW SRM 53-10-04 FIG 114. HFEC (FLAT SURFACSDR UIEA01062Skin · crackedDURING HFEC INSPECTION, FOUND THE LOWER AFT CARGO COMPARTMENT DOOR CUT-OUT, UPPER FORWARD CORNER SKIN CRACKED. CRACK TRIMMED AWAY. FILLER AND REPAIR DOUBLERS FABRICATED AND INSTALLED PER STANDARD PRACTICES IAW SRM 53-30-03 FIG 60, TYPE II. REINSPECTION IS RSDR USAA010848Beam · corrodedPIT - FOUND BEAM CORRODED IN THREE AREAS 1 INCH BY 1 INCH, STATION 208.1 RIGHT UNDER GALLEY NR 1. CORROSION LEVEL 1, TASK NR C53-107-01. CLEANED AND TREATED PER C/N 53-46-53500-C-005. (M)SDR AALA20011344Skin · gougedTUL - FOUND FUSELAGE SKIN GOUGED STATION 237 LONGERON 20L. CUT OUT 1 INCH HOLE TOO REMOVE DAMAGE AND INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)SDR AALA20011388SkinTUL - FOUND LIGHTNING STRIKES IN FUSELAGE SKIN STATION 473 TO 481 LONGERON 7 LEFT. INSTALLED DOUBLER PER SRM 53-04 FIG 38 SHEET 24-36-37-38. (M)
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